Page 400 - Cam Design Handbook
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THB12  9/19/03  7:34 PM  Page 388

          388                      CAM DESIGN HANDBOOK

                                            1  ds
                                     tana =      .
                                           R  q () d q
          Thus the nominal follower velocity is
                                       ˙ s = w R( tan)a                (12.21)

          where w is the constant input angular velocity of the shaft. Integrating Eq. (12.21) gives
          the nominal displacement at the roller
                                         t
                                    s = w  R() q tan a dt.             (12.22)
                                        Ú 0
          The equivalent stiffness k eq of the system is derived in Koster (1975).
                                     1   1  1
                                                 2
                                       =   +  tan a                    (12.23)
                                    k    k  k
                                     eq  c   t
          where k eq, the equivalent vertical spring stiffness, is
                                            kk
                                       k =    x
                                        c
                                            +
                                           kk
                                              x
          and k c, the equivalent tangential spring stiffness, is
                                           kk
                                       k =  y q  .
                                        c
                                           k +  k
                                           y  q
          k eq thus obtained is time-dependent.
             The original model with four degrees of freedom may be approximated by a model
          with a single degree of freedom with variable stiffness, using the general application for
          the rule of transformation. The equation of motion of the system
                                   ˙˙ + (
                                       ˙ -
                                                -
                                 mx c s x ˙)+  k ( s x) = 0
                                             eq
          where the dots represent differentiation with respect to time.
             Using Eq. (12.23) gives
                                            k
                                                    -
                                  ˙ -
                            mx c s x ˙)+     c    ( sx) = 0 .          (12.24)
                              ˙˙ + (
                                          k Ê 1  ˆ  2
                                        1 +  c  s ˙
                                          k t  Ë w R  ¯
          The effect of the flexibility of the shaft is greatest for the position of the cam correspon-
          ding to a = a max. For many cam profiles this occurs at the midpoint of the cam. As a first
          approximation, R(q) can be replaced by the mean pitch radius of the cam
                                        R q () =  R .                  (12.25)
                                              m
          Eq. (12.24) can now be rewritten as
                                            k
                            mx c s x ˙)+     c    2  ( sx) = 0 .       (12.26)
                                                     -
                                  ˙ -
                             ˙˙ + (
                                          k Ê 1  ˆ
                                       1 +  c  Á  s ˙˜
                                          k Ë w R m  ¯
                                          1
          Next, the following nondimensional parameters are introduced:
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